CA2591231A1 - Dual pressure euler steam turbine - Google Patents
Dual pressure euler steam turbine Download PDFInfo
- Publication number
- CA2591231A1 CA2591231A1 CA002591231A CA2591231A CA2591231A1 CA 2591231 A1 CA2591231 A1 CA 2591231A1 CA 002591231 A CA002591231 A CA 002591231A CA 2591231 A CA2591231 A CA 2591231A CA 2591231 A1 CA2591231 A1 CA 2591231A1
- Authority
- CA
- Canada
- Prior art keywords
- rotor
- steam
- pressure
- combination
- passages
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
- F01D1/02—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
- F01D1/06—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines traversed by the working-fluid substantially radially
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/04—Blade-carrying members, e.g. rotors for radial-flow machines or engines
- F01D5/041—Blade-carrying members, e.g. rotors for radial-flow machines or engines of the Ljungström type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/31—Application in turbines in steam turbines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/30—Arrangement of components
- F05D2250/31—Arrangement of components according to the direction of their main axis or their axis of rotation
- F05D2250/315—Arrangement of components according to the direction of their main axis or their axis of rotation the main axis being substantially vertical
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
Abstract
A turbine, including a rotor on a shaft, and having in combination stationary nozzles discharging steam at a first pressure or pressures thereby producing impulse forces on the rotor; internal passages in the rotor producing a pressure head increase in the discharged steam, while simultaneously accelerating the steam, the steam discharged to a second pressure lower than the first pressure, producing reaction forces on the rotor; seal means between the stationary nozzles and the rotor, maintaining the pressure difference between the first pressure and the second pressure while minimizing steam leakage past the internal passages, turbine operations producing shaft power.
Claims (14)
1. A turbine, including a rotor on a shaft having an axis, and having in combination:
a) stationary nozzles discharging steam at a first pressure or pressures thereby producing impulse forces on said rotor, b) the rotor having blades forming internal passages producing a pressure head increase in the discharged steam, while simultaneously accelerating the steam, the steam discharged to a second pressure lower than the first pressure, producing reaction forces on the rotor, c) seal means between the stationary nozzles and the rotor, maintaining the pressure difference between the first pressure and the second pressure while minimizing steam leakage past the internal passages, said seal means carried by the rotor and oriented in a radial, direction relative to said axis to seal against non-rotating nozzle surface or surfaces to restrict steam flow that would otherwise bypass said passages formed by the rotor blades, d) turbine operation producing shaft power, e) and including passages in the rotor between the blades configured to centrifuge liquid and/or solid particles in the steam directionally away from passage inlets, f) each said rotor blade, in cross section, having surfaces configured to define converging passages between said rotor blades causing an increase in fluid pressure above said first pressure such that flow pressure in the passages increases to a maximum value greater than said first pressure and then decreases to a pressure less than said first pressure.
a) stationary nozzles discharging steam at a first pressure or pressures thereby producing impulse forces on said rotor, b) the rotor having blades forming internal passages producing a pressure head increase in the discharged steam, while simultaneously accelerating the steam, the steam discharged to a second pressure lower than the first pressure, producing reaction forces on the rotor, c) seal means between the stationary nozzles and the rotor, maintaining the pressure difference between the first pressure and the second pressure while minimizing steam leakage past the internal passages, said seal means carried by the rotor and oriented in a radial, direction relative to said axis to seal against non-rotating nozzle surface or surfaces to restrict steam flow that would otherwise bypass said passages formed by the rotor blades, d) turbine operation producing shaft power, e) and including passages in the rotor between the blades configured to centrifuge liquid and/or solid particles in the steam directionally away from passage inlets, f) each said rotor blade, in cross section, having surfaces configured to define converging passages between said rotor blades causing an increase in fluid pressure above said first pressure such that flow pressure in the passages increases to a maximum value greater than said first pressure and then decreases to a pressure less than said first pressure.
2. The combination of claim 1 wherein the rotor consists essentially of titanium alloy for erosion resistance.
3. The combination of claim 2 wherein certain of said seal means are provided at the same diametric location on opposite sides of the rotor to produce a force balance on the rotor.
4. The combination of claim 1 wherein holes are provided at locations radially inward from said passages, to enable steam from one side of the rotor to translate to the other side of the rotor, to produce a balance force on the rotor.
5. The combination of, claim 1 where passages are provided radially outwardly of the rotor to enable steam flow from one side to the other side of the rotor to produce a force balance on the rotor.
6. The combination of claim 1 having a shaft seal characterized in that pressurized gas provides a means to prevent leakage of steam to the surroundings and wherein non-contact structural faces providing centrifugal forces are used to reduce pressurized gas leakage into the steam.
7. The combination of 1 in which additional rows of stationary nozzles, rotor passages and seal means are provided on the same rotor and oriented in radially outward directions to enable additional power producing steam expansions.
8. The combination of claim 1 wherein the turbine shaft drives gearing which drives an electric generator at synchronous speed to produce electric power from the steam energy.
9. The combination of claim 1 wherein the turbine shaft directly drives a high speed electric generator at a speed above synchronous speed producing electric power from the steam energy.
10. The combination of claim 1 wherein the turbine shaft drives a pump.
11. The combination of claim 1 wherein the turbine shaft drives a compressor.
12. The combination of claim 8 wherein control means and electrical means are provided to produce a complete, automated and self-regulated system to produce electric power from steam energy and to enable ease of installation.
13. The combination of Claim 8 wherein the rotor shaft, gearing shaft and generator shaft are vertically oriented to enable a compact assembly.
14. The combination of claim 1 wherein control means and electrical means are provided to produce a complete, automated and self-regulated system to produce electric power from steam energy and to enable ease of installation.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/013,073 US7244095B2 (en) | 2004-12-16 | 2004-12-16 | Dual pressure Euler steam turbine |
US11/013,073 | 2004-12-16 | ||
PCT/US2005/041897 WO2006065445A2 (en) | 2004-12-16 | 2005-11-18 | Dual pressure euler steam turbine |
Publications (2)
Publication Number | Publication Date |
---|---|
CA2591231A1 true CA2591231A1 (en) | 2006-06-22 |
CA2591231C CA2591231C (en) | 2010-01-26 |
Family
ID=36588336
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA2591231A Expired - Fee Related CA2591231C (en) | 2004-12-16 | 2005-11-18 | Dual pressure euler steam turbine |
Country Status (4)
Country | Link |
---|---|
US (1) | US7244095B2 (en) |
EP (1) | EP1828542B1 (en) |
CA (1) | CA2591231C (en) |
WO (1) | WO2006065445A2 (en) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101454456B1 (en) * | 2007-04-30 | 2014-11-03 | 누보 피그노네 에스피에이 | Method and system for turbine blade characterization |
GB0800451D0 (en) * | 2008-01-11 | 2008-02-20 | Cummins Turbo Tech Ltd | A turbomachine system and turbine therefor |
US8079802B2 (en) * | 2008-06-30 | 2011-12-20 | Mitsubishi Heavy Industries, Ltd. | Gas turbine |
US8079803B2 (en) * | 2008-06-30 | 2011-12-20 | Mitsubishi Heavy Industries, Ltd. | Gas turbine and cooling air supply structure thereof |
CN101493016B (en) * | 2008-12-10 | 2011-05-11 | 上海电气电站设备有限公司 | Single-cylinder, reaction and impulse turbine |
US8814499B2 (en) * | 2010-04-19 | 2014-08-26 | Korea Fluid Machinery Co., Ltd. | Centrifugal compressor |
US20130142638A1 (en) | 2010-05-28 | 2013-06-06 | Teruhiko Ohbo | Radial flow steam turbine |
US20120006024A1 (en) * | 2010-07-09 | 2012-01-12 | Energent Corporation | Multi-component two-phase power cycle |
US20120063874A1 (en) * | 2010-09-15 | 2012-03-15 | Applied Materials, Inc. | Low profile dual arm vacuum robot |
ITMI20110684A1 (en) | 2011-04-21 | 2012-10-22 | Exergy Orc S R L | PLANT AND PROCESS FOR ENERGY PRODUCTION THROUGH ORGANIC CYCLE RANKINE |
US8701410B1 (en) * | 2011-05-20 | 2014-04-22 | Mark W. Miles | Ballistic impulse turbine and method |
EP2770164A1 (en) | 2013-02-22 | 2014-08-27 | Geislataekni ehf | A turbine having a radial outflow rotor and radial inflow stator |
HUE050519T2 (en) | 2014-05-05 | 2020-12-28 | Exergy Int S R L | Radial turbomachine |
CN110307041B (en) * | 2019-06-24 | 2024-03-26 | 中信重工机械股份有限公司 | Steam sealing device at end part of steam turbine based on centrifugal compression principle |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1359227A (en) * | 1918-12-11 | 1920-11-16 | Universal Turbine Company | Steam-turbine |
US1860817A (en) * | 1928-10-03 | 1932-05-31 | Laval Steam Turbine Co | Rotary pump |
US2021078A (en) * | 1933-11-08 | 1935-11-12 | Andrew S Miller | Turbine |
US3038318A (en) * | 1957-06-07 | 1962-06-12 | Sulzer Ag | Expansion turbine and turbocompressor connected therewith in a cold producing plant |
US3083448A (en) * | 1957-12-11 | 1963-04-02 | Ici Ltd | Articles with erosion-resistant surfaces |
US3038138A (en) * | 1959-01-30 | 1962-06-05 | Engelhard Ind Inc | Collector ring assembly |
US3083318A (en) * | 1959-04-27 | 1963-03-26 | Frank E Hanscom | Brushes with means for neutralizing static charges |
US3044837A (en) * | 1959-09-03 | 1962-07-17 | Whiton Machine Company | Turbine construction |
US3314647A (en) * | 1964-12-16 | 1967-04-18 | Vladimir H Pavlecka | High energy conversion turbines |
US4687946A (en) * | 1972-04-26 | 1987-08-18 | Westinghouse Electric Corp. | System and method for operating a steam turbine with digital computer control and with improved monitoring |
US3966351A (en) * | 1974-05-15 | 1976-06-29 | Robert Stanley Sproule | Drag reduction system in shrouded turbo machine |
JPS6014915B2 (en) * | 1977-04-22 | 1985-04-16 | 株式会社日立製作所 | water pressure balance device |
DE3300864C1 (en) * | 1983-01-13 | 1984-03-22 | Aktiengesellschaft Kühnle, Kopp & Kausch, 6710 Frankenthal | Removal of dirt particles in radial turbines |
FR2611228B1 (en) * | 1987-02-20 | 1990-05-25 | Boussuges Pierre | CENTRIFUGAL ACTION TURBINE |
DE69529178T2 (en) * | 1995-09-13 | 2003-10-02 | Toshiba Kawasaki Kk | METHOD FOR PRODUCING A TITANIUM ALLOY TURBINE BLADE AND TITANIUM ALLOY TURBINE BLADE |
JP3567064B2 (en) * | 1997-06-23 | 2004-09-15 | 株式会社 日立インダストリイズ | Labyrinth seal device and fluid machine provided with the same |
-
2004
- 2004-12-16 US US11/013,073 patent/US7244095B2/en active Active
-
2005
- 2005-11-18 EP EP05849452.7A patent/EP1828542B1/en active Active
- 2005-11-18 CA CA2591231A patent/CA2591231C/en not_active Expired - Fee Related
- 2005-11-18 WO PCT/US2005/041897 patent/WO2006065445A2/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2006065445B1 (en) | 2007-01-18 |
US20060133921A1 (en) | 2006-06-22 |
CA2591231C (en) | 2010-01-26 |
EP1828542B1 (en) | 2014-08-27 |
US7244095B2 (en) | 2007-07-17 |
EP1828542A4 (en) | 2012-02-15 |
EP1828542A2 (en) | 2007-09-05 |
WO2006065445A2 (en) | 2006-06-22 |
WO2006065445A3 (en) | 2006-11-23 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EEER | Examination request | ||
MKLA | Lapsed |
Effective date: 20171120 |